Author:
Cao Lu,Yang Weiwei,Li Hengnian,Zhang Zhidong,Shi Jianjun
Funder
National Natural Science Foundation of China
State Key Laboratory of Astronautic Dynamics Foundation
Subject
Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics
Reference29 articles.
1. Cubature Kalman filters;Arasaratnam;IEEE Trans. Automatic Control,2009
2. Gauss and Jacobi Sums;Bernde,1998
3. Biswas, S., Qiao, L., Dempster, A., 2016. A novel a priori state computation strategy for the unscented kalman filter to improve computational efficiency. IEEE Trans. Automatic Control, http://dx.doi.org/10.1109/TAC.2016.2599291.
4. Central difference predictive filter for attitude determination with low precision sensors and model errors;Cao;Adv. Space Res.,2014
5. Vector observations-based gyro-less spacecraft attitude/angular rate estimation using particle filtering;Carmi,2006
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